How to Calculate Density behind oblique shock for given upstream density and normal upstream Mach number?
Density behind oblique shock for given upstream density and normal upstream Mach number calculator uses Density behind shock = Density ahead of shock*((Specific Heat Ratio Dynamic+1)*(Component of upstream mach normal to oblique shock^2)/(2+((Specific Heat Ratio Dynamic-1)*(Component of upstream mach normal to oblique shock^2)))) to calculate the Density behind shock, The Density behind oblique shock for given upstream density and normal upstream Mach number formula is obtained by multiplying density ratio across the oblique shock to the density ahead of the oblique shock. Density behind shock is denoted by ρ _{2} symbol.
How to calculate Density behind oblique shock for given upstream density and normal upstream Mach number using this online calculator? To use this online calculator for Density behind oblique shock for given upstream density and normal upstream Mach number, enter Density ahead of shock (ρ _{1}), Specific Heat Ratio Dynamic (κ) & Component of upstream mach normal to oblique shock (M_{n1}) and hit the calculate button. Here is how the Density behind oblique shock for given upstream density and normal upstream Mach number calculation can be explained with given input values -> 3.752261 = 1.4*((1.392758+1)*(2^2)/(2+((1.392758-1)*(2^2)))).